Features of pressure suit system that will provide thermal protection of worker performing tasks outside space vehicle and emergency pressurization within vehicle; system uses insulated coverall garment with low solar absorptivity outer cover to minimize effects of external environment; problems, requirements, methods, and design for cislunar and lunar surface extravehicular space suit.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Thermal protection system for extravehicular space suits


    Additional title:

    Progress Astronautics Aeronautics


    Contributors:


    Publication date :

    1963


    Size :

    15 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :